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Experimental study on a yawed square cylinder in oscillatory flows

机译:振荡流动越瓦上圆柱体的实验研究

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摘要

The vortical structures around a yawed square cylinder oscillating in quiescent water are investigated using the particle image velocimetry technique. Following a previous study on the hydrodynamics (Lou et al., 2017), the present experiments are performed at different yaw angles (alpha) and Keulegan-Carpenter (KC) numbers to correlate the independence principle (IP) to vortical flow structures. At KC = 6, the vortex pair shows no shedding. Similar vortex patterns at different yaw angles result in similar hydrodynamic behaviors, which validates the IP at small KC numbers. The single and double pairs of vortex shedding regimes are observed for alpha = 0 degrees at KC = 11 and 19, respectively, and the vortex shedding process is determined by the movement of the cylinder as well as the interaction between vortices and shear layers. As alpha increases to 45 degrees, the shear layers are stretched and show attachment to the upper and lower sides of the cylinder for most of the time within one oscillating cycle. The shedding is only observed at the end of each half cycle and the vortices are found to reattach to the cylinder body. The subsequent drag force behavior of the yawed cylinder displays significant differences from that at alpha = 0 degrees and hence the IP is no longer applicable at KC = 11 and 19. When KC increases to 25, a three pairs of vortex shedding regime can be observed at both alpha = 0 degrees and 45 degrees. A similar flow feature, characterized by the shear layer attachment when the cylinder is at the neutral position and the vortex shedding at the end of each half cycle, has been found for both alpha = 0 degrees and 45 degrees. This result indicates that the IP becomes valid for the yawed square cylinder when the KC is sufficiently large until it is analogous to the steady flow.
机译:使用颗粒图像速度技术研究了在静止水中振荡的旋转方圆柱周围的涡流结构。在上一项关于流体动力学的研究之后(Lou等,2017),本实验在不同的偏航角(α)和keulegan-木匠(KC)数处进行,以将独立原理(IP)与涡流结构相关联。在KC = 6时,涡旋对显示没有脱落。不同偏航角的类似涡旋图案导致类似的流体动力行为,其在小KC号上验证IP。在KC = 11和19分别观察到α= 0度的单对涡流脱落制度,并且通过汽缸的移动以及涡流和剪切层之间的相互作用来确定涡旋脱落过程。随着alpha增加到45度,剪切层被拉伸并显示到一个振荡循环内大部分时间的大部分时间内的附着到圆柱的上侧和下侧。仅在每个半周期的末端观察到脱落,并且发现涡流将重新连接到缸体。随后的摇滚圆筒的拖曳力行为显示出与α= 0度的显着差异,因此IP不再适用于KC = 11和19.当KC增加到25时,可以观察到三对涡旋脱落制度。 Alpha = 0度和45度。对于α= 0度和45度,发现当圆柱体处于空档位置时,其特征在于剪切层附件,并且已经发现了α= 0度和45度。该结果表明,当KC足够大时,IP对于摇摆方形圆柱体,直到类似于稳定流动。

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